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005 | 20211102081733.0 | ||
008 | 090715s2008 inuad b 001 0 eng d | ||
011 | _aChanged OCLC from 213382000 to 288987066 | ||
020 | _a9780132272681 (hbk.) | ||
020 | _a0132272687 (hbk.) | ||
035 | _a(ATU)b11450125 | ||
035 | _a(OCoLC)288987066 | ||
040 |
_aUKM _cUKM _dYDXCP _dBAKER _dBWX _dOCLCG _dRUQBL _dGA0 _dATU |
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050 | 4 |
_aTL570 _b.B54 2009 |
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082 | 0 | 4 |
_a629.1323 _222 |
100 | 1 |
_aBertin, John J., _d1938- _9265130 |
|
245 | 1 | 0 | _aAerodynamics for engineers. |
250 |
_a5th ed. / _bJohn J. Bertin. |
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264 | 1 |
_aIndianapolis, Ind. : _bPrentice Hall ; _aLondon : _bPearson Education [distributor], _c2008. |
|
300 |
_axix, 732 p. : _bill. charts ; _c25 cm. |
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500 | _aPrevious ed.: 2002. | ||
504 | _aIncludes bibliographical references and index. | ||
505 | 0 | 0 |
_g1. _tFluid Properties -- _g2. _tFundamentals of Fluid Mechanics -- _g3. _tDynamics of an Incompressible, Inviscid Flow Field -- _g4. _tViscous Boundary Layers -- _g5. _tCharacteristic Parameters for Airfoil and Wing Aerodynamics -- _g6. _tIncompressible Flows Around Airfoils of Infinite Span -- _g7. _tIncompressible Flows About Wings of Finite Span -- _g8. _tDynamics of a Compressible Flow Field -- _g9. _tCompressible, Subsonic Flows and Transonic Flows -- _g10. _tTwo-Dimensional Supersonic Flows Around Thin Airfoil -- _g11. _tSupersonic Flows Over Wings and Airplane Configurations -- _g12. _tHypersonic Flows -- _g13. _tAerodynamic Design Considerations -- _g14. _tTools for Defining the Aerodynamic Environment -- _gAppendix A. _tThe Equations of Motion Written in Conservation Form -- _gAppendix B. _tA Collection of Often Used Tables. |
520 | _a"Revised to reflect the technological advances and modern application in Aerodynamics, the Fifth Edition of Aerodynamics for Engineers merges fundamental fluid mechanics, experimental techniques, and computational fluid dynamics techniques to build a solid foundation for students in aerodynamic applications from low-speed flight through hypersonic flight. It presents a background discussion of each topic followed by a presentation of the theory, and then derives fundamental equations, applies them to simple computational techniques, and compares them to experimental data. ."--Publisher's website. | ||
650 | 0 |
_aAerodynamics. _9313459 |
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907 |
_a.b11450125 _b09-11-17 _c27-10-15 |
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